The numerical simulation and evaluation of aircraft engine axial flow turbine using numerical techniques

Bhavana, G N S and Singh, Suraj and Srinivas, G (2019) The numerical simulation and evaluation of aircraft engine axial flow turbine using numerical techniques. International Journal of Mechanical and Production, 9 (4). pp. 989-994. ISSN 2249-6890

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Abstract

This research aims to improve the efficiency of an axial flow turbine by improving the boundary conditions. In the baseline paper, Sherwood number, Nusselts number for a given flow were determined. The pressure ratio was not considered in the paper

Item Type: Article
Uncontrolled Keywords: Axial Flow Turbines, ANSYS Fluent, Sherwood Number, Nusselt Number, Tip Losses & Efficiency
Subjects: Engineering > MIT Manipal > Aeronautical and Automobile
Depositing User: MIT Library
Date Deposited: 24 Jul 2019 04:52
Last Modified: 24 Jul 2019 04:52
URI: http://eprints.manipal.edu/id/eprint/154226

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